A review of molecular tagging measurement technique

F Li, H Zhang, B Bai - Measurement, 2021 - Elsevier
Molecular tagging measurement technique is an advanced non-intrusive visualization
approach which uses the molecules as the tagging and tracking materials. This technique …

Application of focused laser differential interferometry (FLDI) in a supersonic boundary layer

A Ceruzzi, B Callis, D Weber, CP Cadou - Aiaa scitech 2020 forum, 2020 - arc.aiaa.org
Single-point and two-point focused laser differential interferometry (FLDI) are used to
explore the structure of a turbulent boundary layer in a Mach 2.6 in-draft wind tunnel's test …

[PDF][PDF] 激光诱导荧光技术燃烧诊断的研究进展

朱家健, 万明罡, 吴戈, 闫博, 田轶夫, 冯戎… - Chinese Journal of …, 2021 - researching.cn
摘要激光诱导荧光(LIF) 技术具有非扰动, 实时原位测量, 组分选择性强, 灵敏度好,
时空分辨率高等优点, 可用于燃烧诊断中测量火焰的重要特征参数. 介绍了LIF …

Non-intrusive measurement techniques for flow characterization of hypersonic wind tunnels

PM Danehy, J Weisberger, C Johansen, D Reese… - 2018 - ntrs.nasa.gov
This manuscript describes the wide variety of optical measurement techniques for
characterizing the flow in hypersonic wind tunnels. The introduction briefly describes …

Amplification and structure of streamwise-velocity fluctuations in compression-corner shock-wave/turbulent boundary-layer interactions

MA Mustafa, NJ Parziale, MS Smith… - Journal of Fluid …, 2019 - cambridge.org
In this work, we study the effect of the compression-corner angle on the streamwise turbulent
kinetic energy (sTKE) and structure in Mach 2.8 flow. Krypton tagging velocimetry (KTV) is …

Flow characterization at heated air supersonic facility sbr-50

P Andrews, P Lax, S Elliott, A Firsov, S Leonov - Fluids, 2022 - mdpi.com
The supersonic wind tunnel facility SBR-50 at the University of Notre Dame was built in 2015
for experimental research related to shock wave (SW) interactions with obstacles and …

[HTML][HTML] Application of high-speed self-aligned focusing schlieren system for supersonic flow velocimetry

PA Lax, SB Leonov - Aerospace, 2024 - mdpi.com
A self-aligned focusing schlieren (SAFS) system combines the field of view of a conventional
schlieren system with the defocus blur of a focusing schlieren system away from the object …

Nonintrusive freestream velocity measurement in a large-scale hypersonic wind tunnel

MA Mustafa, NJ Parziale, MS Smith, EC Marineau - AIAA journal, 2017 - arc.aiaa.org
HIGH-SPEED wind tunnels typically rely on pressure and/or temperature measurement and
nozzle-flow calculations to determine the freestream conditions. This practice can require a …

Femtosecond laser electronic excitation tagging velocimetry in a large-scale hypersonic facility

LE Dogariu, A Dogariu, RB Miles, MS Smith… - AIAA journal, 2019 - arc.aiaa.org
Femtosecond laser electronic excitation tagging (FLEET) is a nonintrusive optical diagnostic
technique that has been demonstrated to provide direct measurement of velocity and other …

Profiles of streamwise velocity and fluctuations in a hypersonic turbulent boundary layer using acetone tagging velocimetry

BA Segall, D Shekhtman, A Hameed, JH Chen… - Experiments in …, 2023 - Springer
Acetone tagging velocimetry (ATV) with nominally 1% mole fraction acetone seeding was
conducted in a shock-tunnel-generated hypersonic turbulent boundary layer over a hollow …